Current insulation device for fuel systems
View Patent ↗An electrical insulating device for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges formed by a part ( 13 ) made of insulating material attached to two metal flanges ( 15, 17 ) that allow inserting the device ( 11 ) between two parts of said linear component, said part ( 13 ) being formed by a cylindrical body ( 21 ) with a castellated crown ( 23 ) on its outer side, formed by longitudinal ( 25 ) and transverse ( 27 ) segments, and said metal flanges ( 15, 17 ) having transverse projections ( 31, 33 ) facing the transverse segments ( 27 ) of the castellated crown ( 23 ) for facilitating their attachment by suitable means ( 39 ).
1. An electrical insulation device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges, characterised in that it is formed by a part ( 13 ) made of insulating material attached to two metal flanges ( 15 , 17 ) that allow inserting the device ( 11 ) between two parts of said linear component, said part ( 13 ) being formed by a cylindrical body ( 21 ) with a castellated crown ( 23 ) on its outer side, formed by longitudinal ( 25 ) and transverse ( 27 ) segments, and said metal flanges ( 15 , 17 ) having transverse projections ( 31 , 33 ) facing the transverse segments ( 27 ) of the castellated crown ( 23 ) for facilitating their attachment by suitable means ( 39 ).
2. An electrical insulating device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges according to claim 1 , characterised in that said flanges ( 15 , 17 ) also include a component ( 35 , 37 ) for installing a bonding point.
3. An electrical insulating device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges according to claim 1 , characterised in that the length of the insulating part ( 13 ) is comprised between 25 and 80 mm.
4. An electrical insulating device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges according to claim 1 , characterised in that the fuel system belongs to an aircraft.
5. An electrical insulating device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges according to claim 2 , characterised in that the length of the insulating part ( 13 ) is comprised between 25 and 80 mm.
6. An electrical insulating device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges according to claim 2 , characterised in that the fuel system belongs to an aircraft.
7. An electrical insulating device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges according to claim 3 , characterised in that the fuel system belongs to an aircraft.
8. An electrical insulating device ( 11 ) for a linear component forming part of a fuel system subjected to risks of possible external electrical discharges according to claim 5 , characterised in that the fuel system belongs to an aircraft.